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(2014 LT26)
Classification: Main-belt Asteroid          SPK-ID: 3246971
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 39 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2622482837139792 3.8784e-08  
a 2.544410820399134 2.1624e-08 au
q 1.877143449686184 9.4409e-08 au
i 11.20765943920839 5.6712e-06 deg
node 185.3595031530356 4.2025e-05 deg
peri 156.4961472620184 4.8962e-05 deg
M 100.3156730500329 2.3742e-05 deg
tp 2458587.409156948738
(2019-Apr-13.90915695)
9.8266e-05 TDB
period 1482.447348225267
4.06
1.8898e-05
5.174e-08
d
yr
n .2428416769276691 3.0957e-09 deg/d
Q 3.211678191112085 2.7294e-08 au
  Orbit Determination Parameters
   # obs. used (total)      270  
   data-arc span      13680 days (37.45 yr)  
   first obs. used      1982-08-16  
   last obs. used      2020-01-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51645  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-22 07:17:14  

Additional Information
 Earth MOID = .875635 au 
 Jupiter MOID = 2.24839 au 
 T_jup = 3.369 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.5   n/a E2018N10  
diameter diameter 3.722 km 0.502 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2012ApJ...759L...8M)  
geometric albedo albedo 0.067   0.025 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2012ApJ...759L...8M)  

Alternate Designations
 2014 LT26 = 1982 QD4 = 2010 PC78 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters ]
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